Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
GOX/Sintin
GOX/Sintin propellant. Gaseous oxygen was proposed for use together with the main engine propellant Sintin, synthetic kerosene, in Russian spacecraft maneuvering engine and orientation thrusters. However the collapse of the Soviet Union brought the production of Sintin, and any spacecraft that may have used it, to an end.

Propellant Formulation: GOX/Sintin. Oxidizer Freezing Point: -219 deg C. Oxidizer Boiling Point: -183 deg C. Fuel Density: 0.806 g/cc. Fuel Freezing Point: -73 deg C. Fuel Boiling Point: 147 deg C.

Subtopics
17D15 Korolev GOX/Sintin rocket engine. Buran OMS large verniers. Out of Production. Large verniers for Buran orbital propulsion system 17D11. Uses synthetic kerosene ('Sintin') for high specific impulse. Oxygen is gaseous in system.
Engines: 17D15.
Back to top of page
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact
© / Conditions for Use